(9)
Install the RIGGING PIN (98DNSA20206080) (7) on the pitch transducer unit (6). (Ref. Fig. 413/TASK 27-92-41-991-014)
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(10)
Remove the bolts (17) and the spring rod (19).
(11)
Tighten the nut (20) on the lockwasher (21).
(12)
Install the spring rod (19) and the bolts (17).
(13)
Remove the RIGGING PIN (98DNSA20206080) (7) from the pitch transducer unit (6). (Ref. Fig. 413/TASK 27-92-41-991-014)
(14)
Make sure that the dial test indicator stays on 0 +0.01 mm (+0.0003 in.) -0.01 mm (-0.0003 in.).
(a) If it is not the case:
-do again the adjustment of the spring rod (19) as the rod length has increased because of locking of the nut (20).
(15)
Install the RIGGING PIN (98DNSA20206080) (7) on the pitch transducer unit (6). (Ref. Fig. 413/TASK 27-92-41-991-014)
(16)
Remove the bolts (17) and the spring rod (19).
(17)
Safety the nut (20) to the lockwasher (21) with lockwire-corrosion resistant steel dia. 0.8 mm (0.03 in.).
(18)
Do again the same operations for the other spring rod. NOTE : Do not install the spring rod (19) at this time if you must
____
also install the other rod.
(19)
Install the spring rod (19) and the bolts (17). NOTE : If you have removed the two spring rods (19), install them at
____
their related position.
(20)
Install the washers (16), the nuts (18) and tighten.
(21)
Remove the RIGGING PIN (98DNSA20206080) (7) from the pitch transducer unit (6). (Ref. Fig. 413/TASK 27-92-41-991-014)
(22)
Make sure that the dial test indicator stays at 0 +0.02 mm (+0.0007 in.) -0.02 mm (-0.0007 in.).
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Subtask 27-92-41-720-050
B. Test
(1)
Put the control handle in a nose-up position (3. approximately) then put the control handle in the neutral position. Release the handle.
(2)
Make sure that the dial test indicator stays at 0 +0.05 mm (+0.0019 in.) -0.05 mm (-0.0019 in.). If it is not the case, do again the adjustment of the spring rods.
(3)
Put the control handle in a nose-down position (3. approximately) then put the control handle in the neutral position. Release the handle.
(4)
Make sure that the dial test indicator stays at 0 +0.05 mm (+0.0019 in.) -0.05 mm (-0.0019 in.). If it is not the case, do again the adjustment of the spring rods.
(5)
Safety the nuts (15) with new cotter pins (18) on the nuts (15).
(6)
Remove the RIGGING PIN (98DNSA20206080) from the roll transducer unit (8).
(7)
Move the side stick in the full directions below:
-nose-up and nose-down
-right and left roll.
Make sure that:
-
the parts move freely
-
the parts that move do not catch the electrical harness
-there is no unwanted materials in the side stick.
5. Close-up
________ Subtask 27-92-41-410-063
A. Connection of the Side Stick Pitch Damper
(1)
Install the damper (9) in the bellcrank (11) and the bolt (4).
(2)
Install the washer (3), the nut (2) and tighten.
(3)
Install a new cotter pin (1) on the nut (2).
Subtask 27-92-41-080-056
B. Removal of the Tools
(1)
Remove the TOOL - ARTIFICIAL FEEL RODS (98D27303004000) (5) from the structure of the side stick (10).
(2)
Disconnect the 28 VDC POWER SUPPLY TOOL (355M03200001) from the electrical connector (15) and from the 28 VDC aircraft network.
(3)
Remove the HOLDER - SIDE STICK (98D27303001001) from the side stick assembly.
Subtask 27-92-41-410-064
C. Install the side stick assembly (Ref. TASK 27-92-41-400-001).
SIDE STICK ASSEMBLY - ADJUSTMENT/TEST
_____________________________________
TASK 27-92-41-710-001
Operational Test of the Side Stick Assembly
WARNING : MAKE SURE THAT ALL THE CIRCUITS IN MAINTENANCE ARE ISOLATED BEFORE
_______
YOU SUPPLY ELECTRICAL POWER TO THE AIRCRAFT.
WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROL SURFACES ARE
_______
CLEAR BEFORE YOU PRESSURIZE/DEPRESSURIZE A HYDRAULIC SYSTEM.
1. Reason for the Job
__________________
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本文鏈接地址：A320飛機維護手冊 AMM FLIGHT CONTROLS 飛行操縱9(58)
